Simultaneous Mean and Covariance Correction Filter for Orbit Estimation

This paper proposes a novel filtering design, from a viewpoint of identification instead of the conventional nonlinear estimation schemes (NESs), to improve the performance of orbit state estimation for a space target. First, a nonlinear perturbation is viewed or modeled as an unknown input (UI) cou...

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Detalles Bibliográficos
Autores principales: Wang, Xiaoxu, Pan, Quan, Ding, Zhengtao, Ma, Zhengya
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5982120/
https://www.ncbi.nlm.nih.gov/pubmed/29734764
http://dx.doi.org/10.3390/s18051444

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5982120/
https://www.ncbi.nlm.nih.gov/pubmed/29734764
http://dx.doi.org/10.3390/s18051444

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